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Realization of electromagnetic hydrodynamics (MHD) propulsion by surfaces needs an electromagnetic body force generated in a conductive fluid (such as seawater and plasma, etc.) around the navigation body. Furthermore, the reaction force against the electromagnetic body force could be used to propel. Based on the basic control equations of electromagnetic field and fluid mechanics, the vector control effect has been analyzed by virtue of field intensity and force distribution characteristic on the rotational navigation body, under two different force action areas. Results show that the navigation attitude adjustment could be realized by this control method without changing attacks and propulsion directions. An upward force moment could be achieved by the control model A. Accordingly, both of the pitching moment and yaw moment could be changed by the control model B. Thus, as a new way of propulsion, the MHD propulsion by surfaces offers several advantages, such as high speed, high efficiency, easy operation, high payload etc. Additionally, in this paper, the vector propulsion has been proved to be one of the remarkable advantages for MHD propulsion by surface.
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Keywords:
- propulsion by surface /
- rotational navigation body /
- navigation /
- vector control
[1] Hsiao C T, Pauley L L 1999 J Fluid Eng. 121 3
[2] Wu G L, Yan J 2008 Guang Dong Shipbuilding 4 2(in Chinese) [吴光林, 严谨2008 广东造船4 2]
[3] Gur O, Rosen A 2009 J. Aircraft 46 1
[4] Mei D J, Fan B C, Huang L P 2010 Acta Phys. Sin. 59 6786 (in Chinese)[梅栋杰, 范宝春, 黄乐萍2010 59 6786]
[5] Liu Z K, Zhou B M, Liu H X 2011 Acta Phys. Sin. 60 084701 (in Chinese)[刘宗凯, 周本谋, 刘会星2011 60 084701]
[6] Mason M S, Crowther W J 2004 2nd AIAA Flow Control Conference (Portland: American Institute of Aeronautics and Astronautics) p2210
[7] Kowal H J 2003 Can. Aeronaut. Space J. 48 2
[8] Howse M 2003 Power Eng. 17 35
[9] Landau D, Chase J, Randolph T 2011 J. Spacecraft Rockets, 48 467
[10] Martinez-Sanchez M, Pollard J E 1998 J. Propul. Power 14 688
[11] Schroeder W K 1999 Fuzzy logic autopilot synthesis for a nonlinearly behaved thruster-controlled missile (Arlington: University of Texas at Arlington) pp46–128
[12] Doman D B, Gamble B J, Ngo A D 2007 AIAA Guidance, Navigation, and Control Conference and Exhibit (Hilton Head: American Institute of Aeronautics and Astronautics) p6778
[13] Ridgely D B, Drake D, Triplett L 2007 AIAA Guidance, Navigation, and Control Conference and Exhibit (Hilton Head: American Institute of Aeronautics and Astronautics) p6771
[14] Ju C G, Peng X B, Liu Y 2009 Sci. China Technol. Sc. 39 505 (in Chinese) [琚春光, 彭小波, 刘宇2009 中国科学 E 辑: 技术科学39 505]
[15] Chen Z H, Fan B C, Aubry N 2006 Chinese Phys. Lett. 23 154
[16] Wang M, Xie Y C 2010 Sci. China Technol. Sc. 40 912(in Chinese) [王敏, 解永春2010 中国科学E 辑: 技术科学40 912]
[17] Hua M D, Hamel T, Morin P 2009 IEEE T. Automat. Contr. 54 1837
[18] Xia Y, Fu M 2003 Overview of Flight Vehicle Control-Compound Control Methodology for Flight Vehicles (Berlin: Springer Berlin Heidelberg) pp49-54
[19] Ren Y X, Chen H X 2006 The Basics of Computational Fluid Dynamics (Beijing: Tsinghua University Press) pp13-34 (in Chinese) [任玉新, 陈海昕2006 计算流体力学基础(北京: 清华大学出版社) 第13–34 页]
[20] Liu Z K, Zhou B M, Liu H X 2013 Fluid Dyn. Res. 45 3
[21] Jiang C B, Zhang R L, Ding Z P 2007 Computational Fluid Dynamics(Beijing: China Electric Power Press) pp161-169 (in Chinese) [江春波, 张永良, 丁则平2007 计算流体力学(北京: 中国电力出版社) 第161–169 页]
[22] Joel H F, Milovan P 2002 Computational Methods for Fluid Dynamics (Berlin: Springer-Verlag) pp164–206
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[1] Hsiao C T, Pauley L L 1999 J Fluid Eng. 121 3
[2] Wu G L, Yan J 2008 Guang Dong Shipbuilding 4 2(in Chinese) [吴光林, 严谨2008 广东造船4 2]
[3] Gur O, Rosen A 2009 J. Aircraft 46 1
[4] Mei D J, Fan B C, Huang L P 2010 Acta Phys. Sin. 59 6786 (in Chinese)[梅栋杰, 范宝春, 黄乐萍2010 59 6786]
[5] Liu Z K, Zhou B M, Liu H X 2011 Acta Phys. Sin. 60 084701 (in Chinese)[刘宗凯, 周本谋, 刘会星2011 60 084701]
[6] Mason M S, Crowther W J 2004 2nd AIAA Flow Control Conference (Portland: American Institute of Aeronautics and Astronautics) p2210
[7] Kowal H J 2003 Can. Aeronaut. Space J. 48 2
[8] Howse M 2003 Power Eng. 17 35
[9] Landau D, Chase J, Randolph T 2011 J. Spacecraft Rockets, 48 467
[10] Martinez-Sanchez M, Pollard J E 1998 J. Propul. Power 14 688
[11] Schroeder W K 1999 Fuzzy logic autopilot synthesis for a nonlinearly behaved thruster-controlled missile (Arlington: University of Texas at Arlington) pp46–128
[12] Doman D B, Gamble B J, Ngo A D 2007 AIAA Guidance, Navigation, and Control Conference and Exhibit (Hilton Head: American Institute of Aeronautics and Astronautics) p6778
[13] Ridgely D B, Drake D, Triplett L 2007 AIAA Guidance, Navigation, and Control Conference and Exhibit (Hilton Head: American Institute of Aeronautics and Astronautics) p6771
[14] Ju C G, Peng X B, Liu Y 2009 Sci. China Technol. Sc. 39 505 (in Chinese) [琚春光, 彭小波, 刘宇2009 中国科学 E 辑: 技术科学39 505]
[15] Chen Z H, Fan B C, Aubry N 2006 Chinese Phys. Lett. 23 154
[16] Wang M, Xie Y C 2010 Sci. China Technol. Sc. 40 912(in Chinese) [王敏, 解永春2010 中国科学E 辑: 技术科学40 912]
[17] Hua M D, Hamel T, Morin P 2009 IEEE T. Automat. Contr. 54 1837
[18] Xia Y, Fu M 2003 Overview of Flight Vehicle Control-Compound Control Methodology for Flight Vehicles (Berlin: Springer Berlin Heidelberg) pp49-54
[19] Ren Y X, Chen H X 2006 The Basics of Computational Fluid Dynamics (Beijing: Tsinghua University Press) pp13-34 (in Chinese) [任玉新, 陈海昕2006 计算流体力学基础(北京: 清华大学出版社) 第13–34 页]
[20] Liu Z K, Zhou B M, Liu H X 2013 Fluid Dyn. Res. 45 3
[21] Jiang C B, Zhang R L, Ding Z P 2007 Computational Fluid Dynamics(Beijing: China Electric Power Press) pp161-169 (in Chinese) [江春波, 张永良, 丁则平2007 计算流体力学(北京: 中国电力出版社) 第161–169 页]
[22] Joel H F, Milovan P 2002 Computational Methods for Fluid Dynamics (Berlin: Springer-Verlag) pp164–206
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